Problem 68
Question
The orbits of stars, planets, comets, asteroids, and satellites all have the shape of one of the conic sections. Astronomers use a measure called eccentricity to describe the shape and elongation of an orbital path. For the circle and ellipse, eccentricity e is calculated with the formula \(e=\frac{c}{d},\) where \(c^{2}=\left|a^{2}-b^{2}\right|\) and \(d\) is the larger value of a or b. For a hyperbola, eccentricity e is calculated with the formula \(e=\frac{c}{d},\) where \(c^{2}=a^{2}+b^{2}\) and the value of \(d\) is equal to a if the hyperbola has \(x\) -intercepts or equal to b if the hyperbola has \(y\) -intercepts. A. \(\frac{x^{2}}{36}-\frac{y^{2}}{13}=1\) B. \(\frac{x^{2}}{4}+\frac{y^{2}}{4}=1\) C. \(\frac{x^{2}}{25}+\frac{y^{2}}{16}=1\) D. \(\frac{y^{2}}{25}-\frac{x^{2}}{39}=1\) G. \(\frac{x^{2}}{16}-\frac{y^{2}}{65}=1\) E. \(\frac{x^{2}}{17}+\frac{y^{2}}{81}=1\) F. \(\frac{x^{2}}{36}+\frac{y^{2}}{36}=1\) H. \(\frac{x^{2}}{144}+\frac{y^{2}}{140}=1\) What do you notice about the values of \(e\) for the equations you identified as hyperbolas?
Step-by-Step Solution
VerifiedKey Concepts
Eccentricity
- An eccentricity of \( e = 0 \) indicates a perfect circle.
- For ellipses, \( 0 < e < 1 \), showing varying degrees of elongation.
- Hyperbolas have \( e > 1 \), indicating they are more open.
Ellipses
- An ellipse is defined by two main parameters: the semi-major axis \(a\) and the semi-minor axis \(b\).
- If \(a = b\), the ellipse becomes a circle.
- The further apart the foci, the more elongated the ellipse.
Hyperbolas
- They are defined by the distances between each vertex and their respective foci.
- Unlike ellipses, hyperbolas open along two branches, resembling mirror images.
- The eccentricity \( e \) of a hyperbola is always greater than 1, which helps to quantify its openness.
Circles
- The equation of a circle is \( \frac{x^2}{r^2} + \frac{y^2}{r^2} = 1 \), where \( r \) is the radius.
- The eccentricity \( e \) of a circle is 0, reflecting the fact it has perfect symmetry and no elongation.
Orbits
- Elliptical orbits, with \( 0 < e < 1 \), are the most common in our solar system, describing paths around the sun and planets.
- Circles \( e = 0 \) are a special case of elliptical orbits with no eccentricity.
- Hyperbolic orbits \( e > 1 \) indicate a celestial body is on a trajectory to leave the gravitational pull of the central body.